Common use of GENERAL CONDITION OF AIRCRAFT AT RETURN Clause in Contracts

GENERAL CONDITION OF AIRCRAFT AT RETURN. 23.9.1 The Aircraft, Engines, APU and Parts will have been maintained and repaired in accordance with the Maintenance Program, the rules and regulations of the Aviation Authority and this Lease. 23.9.2 If any Part installed on the Airframe, any Engine or the APU at return was not installed at Delivery, then such Part will have met the requirements of Article 12.4.1 at the time of installation. 23.9.3 The requirements of Article 12.2.2 will have been met with respect to the installation of PMA Parts and OEM Parts in the Engines during the Lease Term. Without limiting the foregoing, all stationary high energy Parts in the gaspath of the Engines will be OEM Parts. 23.9.4 Aircraft Documentation (including records and manuals) will have been maintained in English and in an up-to-date status, in accordance with the rules and regulations of the Aviation Authority and the FAA and this Lease and in a form necessary in order to meet the requirements of Article 23.8.1. The records and historical documents set forth in Attachment 1 of Exhibit L will be in English. If LESSEE subscribes to Manufacturer’s on-line data access services, LESSEE must nonetheless return the Aircraft manuals with all current revisions provided by Manufacturer in CD, microfilm or other format acceptable to LESSOR. 23.9.5 All hard-time, time-controlled, time-tracked and life-limited Parts which are installed on the Aircraft will have an FAA Form 8130-3 evidencing the airworthiness of such Part at the most recent time of installation on the Aircraft. In the case of life-limited Parts, the documentation will also state the total hours and cycles since new. In the case of hard-time, time-controlled or time-tracked Parts, the documentation will also state the time since last Overhaul or refurbishment, will have a reference to the relevant section of the Component Maintenance Manual under which the Part was Overhauled or refurbished, as applicable, and will identify the FAA-approved repair agency or EASA-approved repair agency, as applicable, which performed the last Overhaul or refurbishment. 23.9.6 All Parts other than those referred to in Article 23.9.5 installed on the Aircraft will have FAA-acceptable documentation demonstrating that such Parts were airworthy at the most recent time of installation on the Aircraft.